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The Enstrom F-28F is equipped with a Lycoming HIO-360-F1AD engine. HIO-360-A1A 180 hp (134 kW) at 2900 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.70:1. Same as the IO-360-A1A except that it has a Bendix RSA-5AB1 fuel injector, Bendix S4LN-200 magnetos and lacks provision for propeller governor drive. [4] HIO-360-A1B
The Lycoming O-360 is a family of four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engines. Engines in the O-360 series produce between 145 and 225 hp (110 and 170 kW), with the basic O-360 producing 180 hp (130 kW).
Lycoming Engines is a major American manufacturer of aircraft engines. With a factory in Williamsport, Pennsylvania , Lycoming produces a line of horizontally opposed , air-cooled, four, six and eight-cylinder engines including the only FAA -certified aerobatic and helicopter piston engines on the market.
Uses a TCM 639231A3 fuel injector. Same as the IO-360-C except for crankshaft counterweight tuning. The crankshaft has one 6th and one 4½ order damper. [4] IO-360-GB 210 hp (157 kW) at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-G except for modified crankshaft.
The design is officially designated the Superior Air Parts O-360 and IO-360. Vantage is a marketing name. [1] [2] The company is owned by the Chinese company Superior Aviation Beijing, which is 60% owned by Chairman Cheng Shenzong and 40% owned by Beijing E-Town, an economic development agency of the municipal government of Beijing.
Pages in category "Lycoming aircraft engines" ... Lycoming IO-233; Lycoming IO-390; ... List of Lycoming O-360 variants;
Prototype with a 120 kW (160 hp) Lycoming O-320 engine FA-200-160 Initial version, powered by 120 kW Lycoming O-320 engine and fixed-pitch propeller. FA-200-180 More powerful development - 130 kW (180 hp) Lycoming IO-360 engine and constant speed propeller. FA-200-180AO Powered by 130 kW Lycoming IO-320 engine and fitted with fixed-pitch propeller.
The type certification for the P.68 Victor, a twin piston engine, high wing monoplane with fixed tricycle landing gear was applied for on 22 January 1969. [2] The Partenavia P.68 was designed as a six-seat light transport and trainer powered by two 200 hp (149 kW) Lycoming IO-360 engines, it made its first flight on 25 May 1970 at Naples. [1]